DE602005021599D1 - Component with thermal insulation layer and method for its production. - Google Patents

Component with thermal insulation layer and method for its production.

Info

Publication number
DE602005021599D1
DE602005021599D1 DE602005021599T DE602005021599T DE602005021599D1 DE 602005021599 D1 DE602005021599 D1 DE 602005021599D1 DE 602005021599 T DE602005021599 T DE 602005021599T DE 602005021599 T DE602005021599 T DE 602005021599T DE 602005021599 D1 DE602005021599 D1 DE 602005021599D1
Authority
DE
Germany
Prior art keywords
production
component
insulation layer
thermal insulation
thermal
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Active
Application number
DE602005021599T
Other languages
German (de)
Inventor
Taiji Torigoe
Ikuo Okada
Katsumi Namba
Kazutaka Mori
Wei Pan
Qiang Xu
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Tsinghua University
Mitsubishi Heavy Industries Ltd
Original Assignee
Tsinghua University
Mitsubishi Heavy Industries Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Tsinghua University, Mitsubishi Heavy Industries Ltd filed Critical Tsinghua University
Publication of DE602005021599D1 publication Critical patent/DE602005021599D1/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12—Blades
    • F01D5/28—Selecting particular materials; Particular measures relating thereto; Measures against erosion or corrosion
    • F01D5/288—Protective coatings for blades
    • C—CHEMISTRY; METALLURGY
    • C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C28/00—Coating for obtaining at least two superposed coatings either by methods not provided for in a single one of groups C23C2/00 - C23C26/00 or by combinations of methods provided for in subclasses C23C and C25C or C25D
    • C23C28/30—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer
    • C23C28/32—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one pure metallic layer
    • C23C28/321—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one pure metallic layer with at least one metal alloy layer
    • C23C28/3215—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one pure metallic layer with at least one metal alloy layer at least one MCrAlX layer
    • C—CHEMISTRY; METALLURGY
    • C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C28/00—Coating for obtaining at least two superposed coatings either by methods not provided for in a single one of groups C23C2/00 - C23C26/00 or by combinations of methods provided for in subclasses C23C and C25C or C25D
    • C23C28/30—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer
    • C23C28/34—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one inorganic non-metallic material layer, e.g. metal carbide, nitride, boride, silicide layer and their mixtures, enamels, phosphates and sulphates
    • C23C28/345—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one inorganic non-metallic material layer, e.g. metal carbide, nitride, boride, silicide layer and their mixtures, enamels, phosphates and sulphates with at least one oxide layer
    • C23C28/3455—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one inorganic non-metallic material layer, e.g. metal carbide, nitride, boride, silicide layer and their mixtures, enamels, phosphates and sulphates with at least one oxide layer with a refractory ceramic layer, e.g. refractory metal oxide, ZrO2, rare earth oxides or a thermal barrier system comprising at least one refractory oxide layer
    • C—CHEMISTRY; METALLURGY
    • C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C30/00—Coating with metallic material characterised only by the composition of the metallic material, i.e. not characterised by the coating process
    • C—CHEMISTRY; METALLURGY
    • C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C4/00—Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge
    • C23C4/04—Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge characterised by the coating material
    • C23C4/10—Oxides, borides, carbides, nitrides or silicides; Mixtures thereof
    • C23C4/11—Oxides
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2230/00—Manufacture
    • F05D2230/90—Coating; Surface treatment
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2300/00—Materials; Properties thereof
    • F05D2300/60—Properties or characteristics given to material by treatment or manufacturing
    • F05D2300/611—Coating
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
DE602005021599T 2004-12-14 2005-12-13 Component with thermal insulation layer and method for its production. Active DE602005021599D1 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP2004361026 2004-12-14

Publications (1)

Publication Number Publication Date
DE602005021599D1 true DE602005021599D1 (en) 2010-07-15

Family

ID=35613915

Family Applications (1)

Application Number Title Priority Date Filing Date
DE602005021599T Active DE602005021599D1 (en) 2004-12-14 2005-12-13 Component with thermal insulation layer and method for its production.

Country Status (4)

Country Link
US (1) US7859100B2 (en)
EP (2) EP1674663B1 (en)
CA (1) CA2529781C (en)
DE (1) DE602005021599D1 (en)

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EP1806430A1 (en) * 2006-01-09 2007-07-11 Siemens Aktiengesellschaft Ceramic layer having high porosity, use of this layer and component comprising such a layer
JP4959213B2 (en) * 2006-03-31 2012-06-20 三菱重工業株式会社 Thermal barrier coating member and manufacturing method thereof, thermal barrier coating material, gas turbine, and sintered body
GB2439312A (en) * 2006-06-20 2007-12-27 Siemens Ag Protective coating for turbine components
US20080044663A1 (en) * 2006-08-18 2008-02-21 United Technologies Corporation Dual layer ceramic coating
KR100798478B1 (en) * 2006-08-31 2008-01-28 한양대학교 산학협력단 Thermal barrier coated materials, method of preparation thereof, and method of coating using them
FR2902693A1 (en) * 2006-12-22 2007-12-28 Siemens Ag Laminate for gas turbine blades or thermal shield, comprises a substrate, an attachment layer, a zirconium oxide layer stabilized by yttrium, an inner ceramic layer on the metallic attachment layer, and an outer ceramic layer
FR2902691A1 (en) * 2006-12-22 2007-12-28 Siemens Ag Laminate for gas turbine blades or thermal shield, comprises a substrate, an attachment layer, a zirconium oxide layer stabilized by yttrium, an inner ceramic layer on the metallic attachment layer, and an outer ceramic layer
FR2902692A1 (en) * 2006-12-22 2007-12-28 Siemens Ag Laminate for gas turbine blades or thermal shield, comprises a substrate, an attachment layer, a zirconium oxide layer stabilized by yttrium, an inner ceramic layer on the metallic attachment layer, and an outer ceramic layer
EP2233450A1 (en) * 2009-03-27 2010-09-29 Alstom Technology Ltd Multilayer thermal protection system and its use
JP5285486B2 (en) * 2009-03-30 2013-09-11 三菱重工業株式会社 Thermal barrier coating material, thermal barrier coating, turbine component and gas turbine
JP5075880B2 (en) * 2009-06-30 2012-11-21 株式会社日立製作所 Heat-resistant parts and high-temperature parts for gas turbines
US9194243B2 (en) * 2009-07-17 2015-11-24 Rolls-Royce Corporation Substrate features for mitigating stress
FR2948690B1 (en) * 2009-07-30 2013-03-08 Snecma PIECE COMPRISING A SUBSTRATE CARRYING A CERAMIC COATING LAYER
US20110143043A1 (en) * 2009-12-15 2011-06-16 United Technologies Corporation Plasma application of thermal barrier coatings with reduced thermal conductivity on combustor hardware
WO2011085376A1 (en) 2010-01-11 2011-07-14 Rolls-Royce Corporation Features for mitigating thermal or mechanical stress on an environmental barrier coating
US8337996B2 (en) * 2010-11-22 2012-12-25 General Electric Company Vanadium resistant coating system
US8678644B2 (en) 2011-08-16 2014-03-25 General Electric Company Hot gas path measurement
US20130224453A1 (en) * 2012-02-29 2013-08-29 United Technologies Corporation Spallation-Resistant Thermal Barrier Coating
CN102674455B (en) * 2012-04-17 2014-10-29 北京理工大学 Rare earth samarium zirconate nano material and hydrothermal preparation method thereof
US9181877B2 (en) 2012-09-27 2015-11-10 United Technologies Corporation Seal hook mount structure with overlapped coating
KR20150060960A (en) * 2012-10-05 2015-06-03 지멘스 악티엔게젤샤프트 Method for treating a gas turbine blade and gas turbine having said blade
WO2014144152A1 (en) 2013-03-15 2014-09-18 Rolls-Royce Corporation Improved coating interface
US9683448B2 (en) 2013-03-18 2017-06-20 Honeywell International Inc. Low conductivity thermal barrier coating
US9316110B2 (en) * 2013-08-08 2016-04-19 Solar Turbines Incorporated High porosity abradable coating
US11479846B2 (en) 2014-01-07 2022-10-25 Honeywell International Inc. Thermal barrier coatings for turbine engine components
DE102014225130A1 (en) * 2014-12-08 2016-06-09 Siemens Aktiengesellschaft Thick thermal barrier coating system
EP3106541A1 (en) * 2015-06-19 2016-12-21 Siemens Aktiengesellschaft Dvc-coating with fully and partially stabilized zirconia
DE102015222808A1 (en) * 2015-11-19 2017-05-24 Siemens Aktiengesellschaft Segmented two-ply layer system
US10578050B2 (en) 2015-11-20 2020-03-03 Tenneco Inc. Thermally insulated steel piston crown and method of making using a ceramic coating
US10519854B2 (en) 2015-11-20 2019-12-31 Tenneco Inc. Thermally insulated engine components and method of making using a ceramic coating
KR101724487B1 (en) * 2015-12-15 2017-04-07 현대자동차 주식회사 Porous thermal insulation coating layer and preparing method for the same
JP6908973B2 (en) * 2016-06-08 2021-07-28 三菱重工業株式会社 Manufacturing methods for thermal barrier coatings, turbine components, gas turbines, and thermal barrier coatings
US10801111B2 (en) 2017-05-30 2020-10-13 Honeywell International Inc. Sintered-bonded high temperature coatings for ceramic turbomachine components
JP2019157216A (en) * 2018-03-14 2019-09-19 三菱重工業株式会社 Ceramic coating, turbine member, gas turbine, and manufacturing method of ceramic coating
US11492298B2 (en) 2018-07-31 2022-11-08 General Electric Company Silicon bond coat with columnar grains and methods of its formation
WO2022035460A1 (en) * 2020-08-14 2022-02-17 Siemens Gas And Power Gmbh & Co. Kg Thermal barrier coating, layered component comprising a thermal barrier coating and gas turbine engine comprising a layered component
CN113403580A (en) * 2021-05-14 2021-09-17 中国航发北京航空材料研究院 Gadolinium samarium zirconium oxygen thermal barrier coating material and preparation method of coating
CN114956810B (en) * 2022-05-19 2023-04-07 陕西天璇涂层科技有限公司 Preparation method of high-toughness phase-change-free low-heat-conductivity tantalate ceramic material

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Also Published As

Publication number Publication date
US20060151856A1 (en) 2006-07-13
EP1959099A3 (en) 2008-10-22
EP1959099B1 (en) 2011-06-15
US7859100B2 (en) 2010-12-28
CA2529781A1 (en) 2006-06-14
EP1959099A2 (en) 2008-08-20
EP1674663B1 (en) 2010-06-02
EP1674663A3 (en) 2006-07-19
CA2529781C (en) 2010-10-12
EP1674663A2 (en) 2006-06-28

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